FR3064739B1 - FLIGHT MANAGEMENT BY ITERATIVE OPTIMIZATION BASED ON A MODEL - Google Patents
FLIGHT MANAGEMENT BY ITERATIVE OPTIMIZATION BASED ON A MODEL Download PDFInfo
- Publication number
- FR3064739B1 FR3064739B1 FR1852788A FR1852788A FR3064739B1 FR 3064739 B1 FR3064739 B1 FR 3064739B1 FR 1852788 A FR1852788 A FR 1852788A FR 1852788 A FR1852788 A FR 1852788A FR 3064739 B1 FR3064739 B1 FR 3064739B1
- Authority
- FR
- France
- Prior art keywords
- specific aircraft
- flight
- control input
- model
- prescribed
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
- 238000005457 optimization Methods 0.000 title abstract 2
- 238000005259 measurement Methods 0.000 abstract 2
- 238000013178 mathematical model Methods 0.000 abstract 1
- 238000000034 method Methods 0.000 abstract 1
Classifications
-
- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/003—Flight plan management
- G08G5/0039—Modification of a flight plan
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/10—Simultaneous control of position or course in three dimensions
- G05D1/101—Simultaneous control of position or course in three dimensions specially adapted for aircraft
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/0005—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with arrangements to save energy
-
- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/0017—Arrangements for implementing traffic-related aircraft activities, e.g. arrangements for generating, displaying, acquiring or managing traffic information
- G08G5/0021—Arrangements for implementing traffic-related aircraft activities, e.g. arrangements for generating, displaying, acquiring or managing traffic information located in the aircraft
-
- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/0017—Arrangements for implementing traffic-related aircraft activities, e.g. arrangements for generating, displaying, acquiring or managing traffic information
- G08G5/0026—Arrangements for implementing traffic-related aircraft activities, e.g. arrangements for generating, displaying, acquiring or managing traffic information located on the ground
-
- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/003—Flight plan management
- G08G5/0034—Assembly of a flight plan
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Automation & Control Theory (AREA)
- Traffic Control Systems (AREA)
- Feedback Control In General (AREA)
Abstract
Un système, support lisible informatiquement, et un procédé incluant d'obtenir des données de vol pour un aéronef spécifique pour un vol prescrit ; d'obtenir des mesures d'échantillons courantes d'au moins un état ou sortie de l'aéronef spécifique ; de réaliser en fonction des données de vol obtenues, des mesures courante ou sorties, et d'un modèle mathématique représentant précisément une performance opérationnelle réelle de l'aéronef spécifique et fournissant une indication prévisionnelle d'une performance future de l'aéronef spécifique, une optimisation de contrôle pour déterminer une entrée de contrôle optimale du point de vue coût pour le vol prescrit ; de régler, en réponse à une considération des caractéristiques opérationnelles réelles de l'aéronef spécifique, l'entrée de contrôle optimisée ; et de transmettre l'entrée de contrôle optimisée réglée à l'aéronef spécifique pour faire fonctionner l'aéronef spécifique pour minimiser le coût de fonctionnement direct pour le vol prescrit.A system, computer readable medium, and method including obtaining flight data for a specific aircraft for a prescribed flight; obtaining current sample measurements of at least one specific aircraft state or output; to perform, based on the flight data obtained, current or output measurements, and a mathematical model precisely representing an actual operational performance of the specific aircraft and providing a predictive indication of a future performance of the specific aircraft, a control optimization to determine a cost-optimal control input for the prescribed flight; adjusting, in response to a consideration of the actual operational characteristics of the specific aircraft, the optimized control input; and transmitting the tuned optimized control input to the specific aircraft to operate the specific aircraft to minimize the cost of direct operation for the prescribed flight.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US15/476,351 US10832581B2 (en) | 2017-03-31 | 2017-03-31 | Flight management via model-based iterative optimization |
US15476351 | 2017-03-31 |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3064739A1 FR3064739A1 (en) | 2018-10-05 |
FR3064739B1 true FR3064739B1 (en) | 2021-04-30 |
Family
ID=63594121
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1852788A Active FR3064739B1 (en) | 2017-03-31 | 2018-03-30 | FLIGHT MANAGEMENT BY ITERATIVE OPTIMIZATION BASED ON A MODEL |
Country Status (3)
Country | Link |
---|---|
US (1) | US10832581B2 (en) |
CN (1) | CN108693889B (en) |
FR (1) | FR3064739B1 (en) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10671092B2 (en) * | 2017-10-20 | 2020-06-02 | The Boeing Company | Airplane climb thrust optimization |
EP3785217A4 (en) | 2018-04-24 | 2021-07-07 | Uber Technologies, Inc. | Determining vtol departure time in an aviation transport network for efficient resource management |
US11238745B2 (en) | 2018-05-07 | 2022-02-01 | Joby Aero, Inc. | Dynamic aircraft routing |
US10593215B2 (en) * | 2018-05-07 | 2020-03-17 | Uber Technologies, Inc. | Dynamic aircraft routing |
FR3090852B1 (en) * | 2018-12-20 | 2020-11-27 | Thales Sa | OPTIMIZATION OF A PARAMETRIC PERFORMANCE MODEL OF AN AIRCRAFT |
FR3090851B1 (en) * | 2018-12-20 | 2021-03-19 | Thales Sa | AUTOMATIC LEARNING IN AVIONICS |
US11900818B2 (en) | 2019-06-10 | 2024-02-13 | Joby Aero, Inc. | Time varying loudness prediction system |
US20210132611A1 (en) * | 2019-11-06 | 2021-05-06 | Uber Technologies, Inc. | Aerial ride quality improvement system using feedback |
US12012229B2 (en) | 2020-03-06 | 2024-06-18 | Joby Aero, Inc. | System and method for robotic charging aircraft |
US20210383706A1 (en) * | 2020-06-05 | 2021-12-09 | Apijet Llc | System and methods for improving aircraft flight planning |
US11814158B1 (en) | 2022-04-28 | 2023-11-14 | Beta Air, Llc | Systems and methods for determining areas of discrepancy in flight for an electric aircraft |
Family Cites Families (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4760530A (en) * | 1986-06-17 | 1988-07-26 | Honeywell Inc. | Flight management system providing minimum total cost |
WO2002099769A1 (en) | 2001-06-01 | 2002-12-12 | The Boeing Company | Air traffic management system and method |
CN101010502A (en) * | 2004-08-27 | 2007-08-01 | 最佳动力技术有限合伙公司 | Predictive engine combustion management |
US7437225B1 (en) | 2005-07-29 | 2008-10-14 | Rockwell Collins, Inc. | Flight management system |
DE102008048275B4 (en) | 2008-09-22 | 2014-07-24 | Airbus Operations Gmbh | Fuel management system |
FR2939917B1 (en) * | 2008-12-12 | 2012-09-21 | Thales Sa | METHOD AND DEVICE FOR OPTIMIZING THE FLIGHT OF AN AIRCRAFT |
CN101937233B (en) * | 2010-08-10 | 2012-05-30 | 南京航空航天大学 | Nonlinear self-adaption control method of near-space hypersonic vehicle |
ITRM20110651A1 (en) | 2010-12-20 | 2012-06-21 | Selex Sistemi Integrati Spa | METHOD OF QUICK PREDICTION OF THE VERTICAL PROFILE OF THE TRAJECTORY FOR THE MANAGEMENT OF AIR TRAFFIC, AND ITS RELATED ATM SYSTEM. |
US8463535B2 (en) | 2011-01-21 | 2013-06-11 | Lockheed Martin Corporation | Method and apparatus for encoding and using user preferences in air traffic management operations |
US20140018980A1 (en) | 2012-07-12 | 2014-01-16 | General Electric Company | Systems and methods for flight management |
CN102981408B (en) * | 2012-12-10 | 2015-05-27 | 华东交通大学 | Running process modeling and adaptive control method for motor train unit |
EP3170166A1 (en) * | 2014-07-18 | 2017-05-24 | The University Of Malta | Flight trajectory optimisation and visualisation tool |
US9625261B2 (en) * | 2014-09-04 | 2017-04-18 | Honeywell International Inc. | System and method for managing speed constraints during required time of arrival operations |
US9946241B2 (en) | 2015-02-23 | 2018-04-17 | Mitsubishi Electric Research Laboratories, Inc. | Model predictive control with uncertainties |
EP3065020B1 (en) * | 2015-03-04 | 2017-10-18 | The Boeing Company | Method for calculating the optimum economy cruise speed in an aircraft |
EP3065019B1 (en) * | 2015-03-04 | 2017-09-13 | The Boeing Company | Method for optimum maximum range cruise speed in an aircraft |
US9536435B1 (en) * | 2015-07-13 | 2017-01-03 | Double Black Aviation Technology L.L.C. | System and method for optimizing an aircraft trajectory |
FR3040801B1 (en) * | 2015-09-09 | 2017-08-25 | Thales Sa | OPTIMIZING THE TRACK OF AN AIRCRAFT |
CN105259904B (en) * | 2015-10-15 | 2018-01-30 | 山东科技大学 | More control surface unmanned plane longitudinal direction decoupling control methods based on Model Predictive Control |
US10460610B2 (en) * | 2016-09-30 | 2019-10-29 | General Electric Company | Aircraft profile optimization with communication links to an external computational asset |
-
2017
- 2017-03-31 US US15/476,351 patent/US10832581B2/en active Active
-
2018
- 2018-03-29 CN CN201810270363.5A patent/CN108693889B/en active Active
- 2018-03-30 FR FR1852788A patent/FR3064739B1/en active Active
Also Published As
Publication number | Publication date |
---|---|
FR3064739A1 (en) | 2018-10-05 |
CN108693889A (en) | 2018-10-23 |
US10832581B2 (en) | 2020-11-10 |
CN108693889B (en) | 2022-05-17 |
US20180286254A1 (en) | 2018-10-04 |
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